# Incident 19960206012729I: Boeing 727247, Portland, OR, February 6, 1996

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: February 6, 1996, 11:52 local time
- Place: Portland, OR
- Airport: Portland International
- Phase of flight: Level Off Touchdown
- Operating rules: Air carrier (Part 121)
- Operator: DALA
- Location: 45.5887° N, 122.5969° W: Placed by OpenAirDocs at PORTLAND INTL (PDX), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=45.5887&lon=-122.5969&mi=10
- Aircraft: N830WA, a cancelled registration (https://openairdocs.org/deregistered/N830WA-2003-12-17) (OpenAirDocs)
- Registry model: Boeing 727-247 (registry code 138408F, https://openairdocs.org/model/boeing-727-247) (OpenAirDocs)
- Registry engine: Pratt & Whitney JT8D-9 series (registry code 52048, https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (OpenAirDocs)
- Reported make and model: BOEING 727247
- People aboard: 111
- Fatal injuries: 0
- Pilot flight hours: 18,000 total, 4,238 in this make and model, 175 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19960206012729I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

NARRATIVE: ON FEBRUARY 6, 1996 AT 1152 PST DELTA FLIGHT 1400 LANDED AT PORTLAND, OREGON ON RUNWAY 28R AND BLEW BOTH RIGHT SIDE MAIN LANDING TIRES. THE RUNWAY WAS CLOSED UNTIL DELTA WAS ABLE TO REMOVE AND REPLACE BOTH TIRES. AT THE TIME OF THE INCIDENT BOTH THE NUMBER 3 ENGINE THRUST REVERSER AND THE ANTI-SKID SYSTEM WERE INOPERATIVE, AND PROPERLY DEFERRED IN ACCORDANCE WITH THE MINIMUM EQUIPMENT LIST. THE CONDITIONS AT THE TIME OF THE INCIDENT WERE HEAVY RAIN AND STANDING WATER. AT THE TIME OF THE INCIDENT RUNWAY 21 WAS IN USE AT PDX, THE CREW RELATED THAT THEY COULD NOT ACCEPT THAT RUNWAY. RUNWAY 28R WAS OFFERED AND ACCEPTED. WINDS WERE 190 @ 21 WITH GUSTS TO 28 KNOTS. UPON LANDING BOTH RIGHT MAIN TIRES BLEW. MAINTENANCE AT PORTLAND REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR TIRES AND BRAKE ASSEMBLIES. IN ADDITION THEY REMOVED AND REPLACED THE ANTI-SKID CONTROL SHIELD. SUBSEQUENT INSPECTION AT PDX REVEALED A CROSSWIRED LEFT MAIN LANDING GEAR ANTI-SKID HARNESS. MAINTENANCE AT PDX REROUTED THE HARNESS, AND OPS CHECKED THE SYSTEM. THEY ALSO REMOVED AND REPLACED #3 THRUST REVERSER PRESSURE SWITCH TO CLEAR THE DMI ON #3 T/R. INFORMED CERTIFICATE HOLDING DISTRICT OFFICE OF FINDINGS.

## Other reports on N830WA (2)

Matched to the same aircraft by N-number and date.

- [Incident 19831112069019I](https://openairdocs.org/incident/19831112069019I), Nov 12, 1983: Boeing 727247 (N830WA), Kansas City, MO. No.1 engine strut overheat lighted on two departures from airport. #1 engine heat detector loop replaced.
- [Incident 19830713043809I](https://openairdocs.org/incident/19830713043809I), Jul 13, 1983: Boeing 727247 (N830WA), Idaho Falls, ID, Substantial damage. Heard a loud bang followed by fire warning on #3 engine. Engine shut down. Found #3 engine front fan disintegrated.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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